# SDR 08FDEA01597

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 25, 2008
- Submitted: April 28, 2008
- Operation: Air carrier
- Aircraft: [N661FE](https://openairdocs.org/aircraft/N661FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 760
- Aircraft time: 19,409 hours, 10,296 cycles
- System (JASC): [5420 · Nacelle/Pylon Miscellaneous Structure](https://openairdocs.org/jasc/5420)
- Part: Panel
- Part number: A546114000000
- Condition: Worn
- Location: Nr 2 Pylon
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/08FDEA01597

## Discrepancy

NR 2 PYLON PANEL NR 423 CL IS WORN FROM FRETTING AT TWO LOCATIONS FRONT AND BACK.  REMOVED DAMAGE REF A300-600 SRM 51-73-10.  ORIGINAL THICKNESS .078.  REMAINING THICKNESS .052.  REMOVED .026.  BEYOND LIMITS REF A300-600 SRM 54-52-51.  FABRICATED DOUBLER AND FILLER REF A300-600 SRM 54-52-51, FIG 203.  CUT OUT DAMAGE REF A300-600 SRM 54-52-51.  ALODINED REF A300-600 SRM 51-21-10.  PRIMED REF A300-600 SRM 51-23-10.  INSTALLED DOUBLER AND FILLER REF A300-600 51-40-21, PARA 5.  PAINTED REF A300-600 SRM 51-23-10.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.